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A Computationally Efficient GNSS/INS Design of Multirotor based on Error-state Kalman Filter
Sheng Wen Cheng
*
, Yi Hsiang Huang
*
此作品的通信作者
臨床醫學研究所
研究成果
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Conference contribution
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引文 斯高帕斯(Scopus)
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Keyphrases
System Design
100%
Computationally Efficient
100%
Inertial Navigation System
100%
Global Navigation Satellite System
100%
Multirotor
100%
Error State Kalman Filter
100%
Inertial Measurement Unit
50%
Systems-based
25%
High Efficiency
25%
Computation Time
25%
On-board Sensors
25%
Symmetric Structure
25%
Code Generator
25%
Computational Resources
25%
Magnetometer
25%
Rangefinder
25%
Update Rate
25%
Flight Computer
25%
Velocity Measurement
25%
Quaternion
25%
System Navigation
25%
Position Measurement
25%
C Code
25%
Sparse Structure
25%
Global Navigation Satellite System Receiver
25%
Unit Bias
25%
Engineering
Kalman Filter
100%
Inertial Navigation System
100%
State Error
100%
Inertial Measurement
50%
Units of Measurement
50%
Computation Time
25%
Symmetric Structure
25%
Computational Resource
25%